N936UW

Part: GIRT BAR — OBSTRUCTED (L4 DOOR SLIDE) · airframe 72,594 hrs · 27,574 cycles

L4 DOOR WILL NOT DISARM. MAINTENANCE FOUND BOTTLE CAP JAMMING GIRT BAR. REMOVED DEBRIS AND ACCOMPLISHED CHECK IAW AMM 52-11-00-862-077.

Part: LINE — DAMAGED (FUEL SYSTEM) · airframe 72,074 hrs · 27,401 cycles

LEFT WING FUEL IMBALANCE WHEN CENTER FUEL USED. IMBALANCE SEEMED TO TERMINATE WHEN CENTER FUEL AT 11,000 LBS. OPERATES NORMAL WITH CENTER FUEL AT 0 AND BALANCED. NO FUEL LEAK PERCIEVED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE AFT CROSSFEED VALVE, FORWARD CROSSFEED VALVE AND THE LEFT FUEL PUMP VAPOR RETURN LINE.

Part: SHUTOFF VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 72,074 hrs · 27,401 cycles

LEFT WING FUEL IMBALANCE WHEN CENTER FUEL USED. IMBALANCE SEEMED TO TERMINATE WHEN CENTER FUEL AT 11,000 LBS. OPERATES NORMAL WITH CENTER FUEL AT 0 AND BALANCED. NO FUEL LEAK PERCIEVED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE AFT CROSSFEED VALVE, FORWARD CROSSFEED VALVE AND THE LEFT FUEL PUMP VAPOR RETURN LINE.

Part: SHUTOFF VALVE — DEFECTIVE (FUEL SYSTEM) · airframe 72,074 hrs · 27,401 cycles

LEFT WING FUEL IMBALANCE WHEN CENTER FUEL USED. IMBALANCE SEEMED TO TERMINATE WHEN CENTER FUEL AT 11,000 LBS. OPERATES NORMAL WITH CENTER FUEL AT 0 AND BALANCED. NO FUEL LEAK PERCIEVED. AIRCRAFT WAS GROUNDED. MAINTENANCE REPLACED THE AFT CROSSFEED VALVE, FORWARD CROSSFEED VALVE AND THE LEFT FUEL PUMP VAPOR RETURN LINE.

Part: GCU — FAILED (LT ENGINE) · airframe 71,931 hrs · 27,353 cycles

LEFT ENGINE GENERATOR FAILED IN FLIGHT AND APU WOULD NOT START IN FLIGHT. APU WAS STARTED ON THE GROUND. THE AIRCRAFT WAS GROUNDED. MAINTENANCE ACCOMPLISHED APU BITE TEST IAW TSM 49-815-846-0-01 WITH NO FAULTS NOTED. MAINTENANCE ALSO REPLACED THE NR 1 GENERATOR CONTROL UNIT (GCU) AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 24-22-02.

Part: COOLING FAN — FAULTY (ZONE 100) · airframe 71,916 hrs · 27,349 cycles

AIRCRAFT WAS NOT GROUNDED: AFTER LANDING, BURNING, HOT ODOR ON ROLLOUT FOLLOWED BY EQUIPMENT COOLING, OVERHEAT LIGHT ON OVERHEAD PANEL AND EICAS MESSAGE, EQUIPMENT OVERHEAT. COMPLETED QRH PROCEDURE DURING TAXI. MAINTENANCE REPLACED THE NR 1 EQUIPMENT COOLING FAN AND ACCOMPLISHED A SATISFACTORY, OPS CHECK IAW AMM 21-58-06-014-001.

Part: SOCKET — BROKEN (CABIN) · airframe 71,916 hrs · 27,349 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT OVER SEAT 3C BROKEN. SOCKET SEPARATED FROM BRACKET. REPAIRED EMERGENCY LIGHT SOCKET AT 3C.

Part: STRING — BROKEN (ZONE 800) · airframe 71,076 hrs · 27,147 cycles

AIRCRAFT IN BASE MX. RT EMER EXIT DOOR, AFT QUICK RELEASE CABLE ASSEMBLY ON DOOR SLIDE PACK TEMPORARY LOOP TIE CHORD, STRING, BROKEN. RETIED R3 DOOR AFT SLIDE RELEASE PIN IAW CMM 25-66-03.

Part: LIGHT — LOOSE (CABIN) · airframe 70,445 hrs · 26,960 cycles

AIRCRAFT WAS NOT GNDED. EMER LIGHT STRIP AT 3L NEEDS TO BE SECURED. SECURED EMER LIGHT STRIP AT 3L.

Part: CASE — CORRODED (NR 1 ENGINE) · airframe 70,262 hrs · 26,916 cycles

AIRCRAFT WAS GNDED. FOUND CORROSION & PITTING ON THE NR 1 ENG FAN CASE, UNDER THE ICE IMPACT PANELS IN VARIOUS PLACES, AROUND ENTIRE ENG. R & R THE NR 1 ENG & ACCOMPLISHED A SATISFACTORY LEAK & OPERATIONAL CHECK IAW TASK CARDS 19L40071001 & 19L40072006.

Part: LIGHT — LOOSE (CABIN) · airframe 69,441 hrs · 26,698 cycles

FLOOR EMER LIGHTING STRIP BY LAVATORY 3R IS LOOSE. SECURED EMER LIGHTING STRIP BY LAVATORY 3R.

Part: LIGHT — LOOSE (CABIN) · airframe 69,441 hrs · 26,698 cycles

FLOOR EMER LIGHTING STRIP BY LAVATORY 3L IS LOOSE. SECURED EMER LIGHTING STRIP BY LAVATORY 3L.

Part: SKIN PANEL — DELAMINATED (TE FLAP) · airframe 68,497 hrs · 26,440 cycles

LEFT WING INBD FLAP, LOWER OTBD SURFACE PANEL 113N2402-41 HAS DELAMINATION. REPLACED FLAP IAW TASK CARD 19L50027003.

Part: WINDOW — CRACKED (COCKPIT) · airframe 67,474 hrs · 26,186 cycles

CAPTAINS FWD WINDOW NR1 CRACKED AT FL 360. REPLACED CAPTAINS FWD WINDOW IAW AMM 56-11-01-424-015.

Part: FLASHLIGHT — INOPERATIVE (FLASHLIGHT) · airframe 66,750 hrs · 25,962 cycles

STEWARDESS SEAT BY L3 DOOR EMER FLASHLIGHT LED INDICATOR LIGHT INOPERATIVE. REPLACED STEWARDESS SEAT EMER FLASHLIGHT BY L3 DOOR.

Part: SLAT — DELAMINATED (LT WING) · airframe 66,067 hrs · 25,727 cycles

C1 CHECK DELAMINATION ON LT WING NR 5 SLAT AT WS 150.5 APPROX 3 INCHES FROM TE. REPLACED LT WING NR 5 SLAT IAW JOB CARD 19C51227001.

Part: FLAP — DELAMINATED (RT WING) · airframe 66,067 hrs · 25,727 cycles

C1 CHECK DELAMINATION ON RT WING INBD TE AFT FLAP AT APPROX 2 INCHES OTBD OF INBD END & 6 INCHES FWD TE. REPLACED RT WING INBD TE AFT FLAP IAW JOB CARD 19L50027002.

Part: LANYARD — DISPLACED (SLIDE RAFT) · airframe 66,000 hrs · 25,713 cycles

RON R1 DOOR SLIDE LANYARD DISPLACED, KEEPS SLIDE FROM FULLY ARMING. R & R R1 DOOR SLIDE IAW JOB CARD 19L80025002.

Part: TRANSMITTER — OUT OF ADJUST (LT WING TE FLAPS) · airframe 63,340 hrs · 24,975 cycles

EN-ROUTE, FLAPS LOCKED OUT AT 20 DEGREE DURING APPROACH, AND WOULD NOT EXTEND OR RETRACT. DID NOT USE ALTERNATE FLAP EXTENSION. THE FLIGHT DID A GO AROUND WHILE THE FLIGHT CREW ATTEMPTED TO CORRECT THE PROBLEM. THE ISSUE COULD NOT BE RESOLVED, SO THE CREW DECLARED AN EMERGENCY, AND RESET THE APPROACH WITH FLAPS 20. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. BITE OF FSLU NR 1 SHOWS LT SLAT TRANSMITTER READING OF LT SLAT TRANSMITTER AT 11.49 WITH FLAPS FULL UP. MAINTENANCE ADJUSTED LT SLAT TRANSMITTER.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 62,132 hrs · 24,631 cycles

DURING CLIMBOUT AT FL300, THE F/O R1 OUTER WINDSHIELD CRACKED WITH A LOUD NOISE. DECLARED AN EMERGENCY AND DID AN EMERGENCY DESCENT TO 10,000 FT. RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED R1 WINDSHIELD.

Part: SENSOR — DIRTY (COCKPIT) · airframe 62,099 hrs · 24,623 cycles

EN-ROUTE, FLIGHT DECK TRIM AIR GOES HOT ON CLIMBOUT (31 DEG C) BURNED OFF AT CRUISE, TURNED TRIM AIR BACK ON, TRIM AIR WENT HOT AGAIN, WITH DISTINCT SMELL OF DUCTWORK. TURNED FLIGHT DECK TRIM AIR OFF, LEFT OFF. MX FOUND COCKPIT TEMP SENSOR EXTREMELY DIRTY. CLEANED SENSOR, OPS CHECKS GOOD.

Part: SLIDE — OUT OF POSITION (L4 DOOR) · airframe 62,069 hrs · 24,611 cycles

L4 DOOR SLIDE DROPPED OUT OF BRACKETS. THE SLIDE WAS REMOVED AND THE ACFT WAS FERRIED, WHERE MX INSTALLED A NEW SLIDE. UNIT WAS DISASSEMBLED, CLEANED, INSPECTED, TESTED & OVERHAULED.

Part: FITTING — LOOSE (CABIN) · airframe 62,057 hrs · 24,606 cycles

4L DOOR -AFT GIRT BAR PAW WILL NOT DISENGAGE ( STAYS IN FLOOR MOUNT) WHEN SLIDE IS DISARMED. FOUND GIRT BAR AND FLOOR FITTING LOOSE AND OUT OF RIG, ADJUSTED FLOOR FITTINGS. DOOR ARMING HANDLE AND LIGHT, OPS CHECK GOOD.

Part: FITTING — LOOSE (CABIN) · airframe 62,057 hrs · 24,606 cycles

"SLIDE" LIGHT ON R1 DOOR NOT ILLUMINATED WHEN SLIDE IN ARMED POSITION. FOUND AFT GIRT BAR FLOOR FITTING LOOSE AND OUT OF RIG. AJUSTED AFT FLOOR FITTING. DOOR ARMING HANDLE AND LIGHT, OPS CKS GOOD.

Part: OVEN — ODOR (GALLEY) · airframe 62,048 hrs · 24,601 cycles

EN-ROUTE, FIRST CLASS OVENS HAVE STRONG OVEN CHEMICAL SMELL. R & R FWD GALLEY OVENS.

Part: SWITCH — INOPERATIVE (CABIN) · airframe 61,993 hrs · 24,584 cycles

C4 CHECK. L2 DOOR EMERGENCY LIGHTS TEST SWITCH INOP. T/S AND FOUND L2 DOOR TEST SWITCH S10293 DEFECT. R & R L2 DOOR SWITCH S10293 & PERFORMED OPS CHECK FOUND NORMAL SWPM 20-84-14, AMM 33-51-00 & WDM 33-51-13.

Part: INDICATOR — BROKEN (R1 DOOR) · airframe 61,993 hrs · 24,584 cycles

C4 CHECK, R-1 DOOR SLIDE LIGHT INDICATOR ABOVE DOOR TRIM IS BROKEN. OPENED R1 DOORWAY PANEL, R & R R1 SLIDE LT ASSY, CLOSED R1 DOORWAY PANEL. R1 GIRT BAR ENGAGEMENT LT (SLIDE LT) L404 TEST NORMAL. REF WDM 25-66-11, AMM 25-21-06 AND 25-66-00.

Part: RESERVOIR — DEPLETED (L2 DOOR) · airframe 61,993 hrs · 24,584 cycles

C4 CHECK, L2 POWER ASSIST RESERVOIR DEPLETED. R & R L2 POWER ASSIST RESERVOIR , REF AMM 52-11-30.

Part: PROXIMITY SENSOR — FAILED (L1 DOOR SLIDE) · airframe 61,993 hrs · 24,584 cycles

C4 CHECK, L1 DOOR , GIRT BAR ENGAGEMENT SLIDE LIGHT TRIPS CIRCUIT BREAKER WHEN SLIDE IS ARMED, LIGHT INOPERATIVE. REPLACED NR 1 PASSENGER DOOR GIRT BAR PROXIMITY SENSOR A 510214 IAW AMM 25-66-11. DOOR GIRT SLIDER INDICATOR LIGHT, OPS CHECKED NORMAL IAW AMM 25-66-11.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 61,993 hrs · 24,584 cycles

C4 CHECK. EMERGENCY EXIT IDENTIFIER ASSY DAMAGED. R & R EMERGENCY EXIT IDENTIFIER ASSY IAW AMM 33-51-10. PERFORMED SIGN TEST. TEST NORMAL.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - THE FOLLOWING EMERGENCY LIGHTS FAILED THE OPS CHECK: AISLE LIGHTS AT ROW 1 RT, ROW 3 RT, ROW 4 LT, ROW 11 RT, ROW 13 LT, 17 LT, ROW 8 RT & ROW 25 RT, R1 DOOR SLIDE LIGHT & R2 & L2 DOOR SLIDE LIGHT. COMPLETED TROUBLESHOOTING OF EMERGENCY LIGHTS & FOUND DEFECTIVE BATTERY POWER SUPPLY M730. REPLACED BATTERY POWER SUPPLY M730 IAW WDM 33-51-21 & 33-51-07. OPS CHECK GOOD.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON R1 DOOR CUTOUT SILL FITTING AT BS333, RBL62. REPLACED R1 DOOR CUTOUT SILL FITTING AT BS333, RBL62 IAW SRM 51-10-02, 51-00-10, 53-01-15 & 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK-LEVEL 2 INTERGRANULAR CORROSION ON L2 DOOR CUT OUT AFT VERTICAL STRUCTURE LOWER ANGLE AT BS730, LBL62. REPAIRED LOWER ANGLE AT BS730, LBL62 IAW SRM 51-10-02, 53-30-15-1A & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK-LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS1640 BETWEEN RBL8 TO LBL54. REPAIRED FLOORBEAM AT BS1640 BETWEEN RBL8 TO LBL54 IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R-3.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT L4 PAX/CREW DOOR CUTOUT BELOW SIL PANEL AT BS1676, LBL62. REPLACED FITTING AT L4 PAX/CREW DOOR CUTOUT BELOW SIL PANEL AT BS1676, LBL62 IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK-LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS365, RBL6. REPAIRED FLOORBEAM AT BS365, RBL6 IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS365 TO BS377, RBL62. REPLACED FLOOR SUPPORT BETWEEN BS365 TO BS377, RBL62 IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FITTING AT R4 PAX/CREW DOOR CUTOUT BELOW SIL PANEL AT BS1676, RBL62. REPLACED FITTING AT R4 PAX/CREW DOOR CUTOUT BELOW SIL PANEL AT BS1676, RBL62 IAW SRM 51-10-02, 53-60-15-1A & 51-40-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM AT BS740, RBL45. REPAIRED FLOORBEAM AT BS740, RBL45 IAW SRM 51-10-02, 53-00-51-1A & 53-00-51-2R.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK-LEVEL 2 GALVANIC CORROSION ON ANGLE SUPPORT BETWEEN BS700 TO BS756, RBL62. REPLACED ANGLE SUPPORT BETWEEN BS700 TO BS756, RBL62 IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FITTING AT L2 DOOR CUT OUT BELOW SIL PANEL AT BS725, LBL64. REPLACED FITTING AT L2 DOOR CUT OUT BELOW SIL PANEL AT BS725, LBL64 IAW SRM 51-10-02, 53-00-51 & 51-40-02.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT, INTERCOSTAL, BETWEEN BS700 TO BS720, LBL62. REPLACED FLOOR SUPPORT, INTERCOSTAL, BETWEEN BS700 TO BS720, LBL62 IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT BETWEEN BS720 TO BS740, RBL62. REPLACED FLOOR SUPPORT BETWEEN BS720 TO BS740, RBL62 IAW B757 SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON ANGLE SUPPORT AT L1 PAX/CREW DOOR CUT OUT LOWER AREA BETWEEN BS365 TO BS377, LBL62. REPLACED ANGLE SUPPORT AT BETWEEN BS365 TO BS377, LBL62 IAW SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FITTING AT L2 DOOR CUT OUT BELOW SIL PANEL AT BS695, LBL62. REPLACED FITTING AT L2 DOOR CUT OUT BELOW SIL PANEL AT BS695, LBL62 IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT JUST INSIDE DOOR R-3 BETWEEN BS1290 TO BS1410, RBL62. REPLACED FLOOR SUPPORT BETWEEN BS1290 TO BS1410, RBL62 IAW SRM 51-40-02.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK-LEVEL 2 EXFOLIATION CORROSION ON SILL WEB AT BS1323, LBL62. REPAIRED SILL WEB AT BS1323, LBL62 IAW SRM 51-10-02 & 51-70-13.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK, LEVEL 2 INTERGRANULAR CORROSION ON FLOOR SUPPORT, INTERCOSTAL, BETWEEN BS720 TO BS740, LBL62. REPLACED FLOOR SUPPORT, INTERCOSTAL, BETWEEN BS720 TO BS740, LBL62 IAW SRM 51-10-02, 53-00-04-1A & 51-40-02.

Part: STIFFENER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON L4 PAX/CREW DOOR CUTOUT AFT VERTICAL STIFFINER AT BS1681, S17L & LBL62. REPLACED VERTICAL STIFFINER AT BS1681, S17L & LBL62 IAW SRM 51-40-02 & DWG 146N8769.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT BS 365, BL 0. REPLACED FLOOR SUPPORT AT BS 365, BL 0 IAW B757 SRM 51-40-02.

Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON FITTING AT R4 DOOR CUTOUT AT BS 1650, RBL 62. REPLACED FITTING AT R4 DOOR CUTOUT AT BS 1650, RBL 62 IAW B757 SRM 51-40-02, 51-10-02-0G & 53-60-15.

Part: SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,991 hrs · 24,583 cycles

C4 CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT AT BS 339, LBL 30. REPLACED SUPPORT AT BS 339, LBL30 IAW B757 SRM 51-10-02, 53-00-51-1A & 51-40-02.

Part: SLAT — DEBONDED (LT WING) · airframe 61,594 hrs · 24,425 cycles

RON VISIT - DISBONDING ON NR 2 SLAT APPROX 38 INCHES FROM OUTBOARD END & 6 INCHES FROM TRAILING EDGE. REPLACED NR 2 SLAT IAW JOB CARD # 19L52027002.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,744 hrs · 24,163 cycles

RON - AFT CARGO FLOOR STRINGER CRACKED AT BS 1460 & RBL 2. DAMAGED SECTION OF FLOORBOARD STRINGER REMOVED, NEW SECTION AND REPAIR PARTS INSTALLED IAW EA 104393.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,744 hrs · 24,163 cycles

RON - AFT CARGO FLOOR STRINGER CRACKED AT BS 1470 & RBL 7. REPAIRED CRACKED STRINGER IAW EA 104393.

Part: UNKNOWN — MALFUNCTIONED (STABILIZER)

CLT FLT 1042 EN-ROUTE BWI TO CLT. STAB TRIM EICAS MESSAGE ON CLIMB. EICAS MESSAGE WENT AWAY AFTER 45 SEC. 60 SEC LATER, WITH A/P ENGAGED AT FL280, A/C PITCHED DOWN. CREW FELT BUMP. 300-400 FPM DESCENT STARTED THEN STOPPED. ON APPROACH, AC PITCHED DOWN WITHOUT A/P ON. HAPPENED THREE TIMES WITH HEAVY NOSE DOWN PRESSURE. MAINTENANCE ACCOMPLISHED HORIZ AND STAB TRIM TEST, STAB TRIM MESSAGE MAN MODE, & ELEV CONTROL SYSTEM TEST. ALL CHECKS OK.

Part: LANYARD — OUT OF POSITION (R1 DOOR) · airframe 60,440 hrs · 24,064 cycles

THE 1R DOOR DIFFICULT TO ARM. FOUND LANYARD FROM SLIDE PACK OBSRTUCTING GIRT FITTINGS FROM ENGAGEMENT. RESTOWED LANYARD. SLIDE ARMS AND UNARMS NORMALLY.

Part: LANYARD — UNSECURE (R1 DOOR) · airframe 60,180 hrs · 23,971 cycles

PHX - 1R DOOR WILL NOT CLOSE. RE-STOWED GIRT BAR LANYARD 1R DOOR. OPS NORMAL.

Part: TRACK — UNSECURE (CABIN) · airframe 60,111 hrs · 23,952 cycles

MCO - ROW 11&12 A/C L EMERGENCY FLOOR STRIP IS LOOSE. INSTALLED EMERGENCY FLOOR STRIP.

Part: SKIN — DEBONDED (LE SLAT) · airframe 59,999 hrs · 23,913 cycles

RON CHECK - DISBOND ON LOWER SURFACE AT INBOARD EDGE OF NR 4 SLAT 6.5 INCHES FORWARD OF TRAILING EDGE WEB. REPLACED NR 4 SLAT IAW B757 AMM 27-81-02-401.

Part: HINGE FITTING — DAMAGED (THRUST REVERSER) · airframe 58,766 hrs · 23,538 cycles

RIGHT OUTBOARD AFT THRUST REVERSER HINGE FITTING HAS PYLON LOWER BOLT HOLES AT PPS 174, PPWL 145. HOLES REAMED AND NEW FITTINGS INSTALLED IAW US AIRWAYS EA 103807B AND US AIRWAYS EO 5408R114 REV C.

Part: LIGHT — UNSECURE (CABIN) · airframe 57,259 hrs · 23,052 cycles

PHL - AISLE "GLOW STRIP" EMERGENCY LIGHTING ON FLOOR-LEFTSIDE-ROW 11 IS COMING UP FROM FLOOR. REPAIRED LUMINESCENT STRIP LOW LEVEL ILLUMINATION STRIP REF LOC ROW 11.

Part: BUSHING — WORN (GIRT BAR) · airframe 57,168 hrs · 23,027 cycles

CLT - DOOR 4L HARD TO ARM APPEARS TO CATCH ON SOMETHING AND THEN GIVEWAY REPORTED BY 2 CREW MEMBERS. REPLACED GIRT BAR LIFTER ASSY BUSHINGS.

Part: AIR FILTER — ODOR (CABIN) · airframe 57,134 hrs · 23,013 cycles

SJU FLT 1032 - EN ROUTE CLT TO SJU. ON DESCENT INTO SJU BURNING PLASTIC FUMES IN CABIN. F/A IN REAR OF A/C COULD TASTE AND SMELL FUMES. THERE WAS NO SMOKE OR HAZE IN CABIN. PERFORMED SMOKE/FIRE/FUMES CHECKLIST, NO INCREASE OR DECREASE OF FUMES NOTED. TROUBLESHOT CABIN AIR QUALITY. NO ODOR NOTED. REPLACED HEPA FILTERS. AIRCRAFT OK FOR SERVICE.

Part: FLAP — DELAMINATED (RT WING) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - DELAMINATION ON RIGHT INBOARD MAIN FLAP 85 INCHES FROM INBOARD END 7 INCHES FROM TRAILING EDGE. REPAIRED RIGHT INBOARD MAIN FLAP IAW B757 SRM 51-70-07.

Part: WEDGE — DEBONDED (LE SLAT) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - DEBONDED AREA ON RIGHT WING NR 6 SLAT TRAILING EDGE WEDGE. REPLACED NR 6 SLAT IAW JOB CARD 19L51027001.

Part: FLAP — DEBONDED (LT WING) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - DISBONDING ON LEFT INBOARD FLAP LOWER TRAILING EDGE APPROX 28 INCHES FROM OUTBOARD END. REPAIRED LEFT INBOARD FLAP LOWER TRAILING EDGE IAW B757 SRM 57-53-01 & 51-70-10.

Part: PANEL — CRACKED (LE SLAT) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - CRACK ON RIGHT WING NR 9 LEADING EDGE SLAT COVE PANEL AT INBOARD DRIVE TRACK. REPAIRED RIGHT WING NR 9 LEADING EDGE SLAT COVE PANEL IAW BOEING DRAWING 114N4076.

Part: PANEL — CRACKED (LE SLAT) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - MULTIPLE CRACKS ON RIGHT WING NR 10 LEADING EDGE SLAT COVE PANEL. REPLACED RIGHT WING NR 10 LEADING EDGE SLAT COVE PANEL IAW BOEING DRAWING NR 114N40756.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - LEVEL 2 EXFOLIATION CORROSION ON WEB INTERCOSTAL BETWEEN BS 1500 AND BS 1520, LBL 2.90. REPLACED WEB INTERCOSTAL BETWEEN BS 1500 AND BS 1520, LBL 2.90 IAW BOEING DRAWING 146N5451.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 57,124 hrs · 23,008 cycles

C3 CHECK - HOLE ON LOWER SIDE OF LEFT OUTBOARD AFT FLAP 6 INCHES INBOARD OF OUTBOARD END & 9 INCHES FROM TRAILING EDGE. REPAIRED LOWER SIDE OF LEFT OUTBOARD AFT FLAP IAW B757 SRM 57-53-01 & 51-70-17 REPAIR 4, FIG 24.

Part: UNKNOWN — MALFUNCTIONED (NLG)

PHL - FLT 1572 EN ROUTE MCO TO PHL. DURING THE APPROACH INTO PHL, THE NLG FAILED TO EXTEND NORMALLY. THE ALTERNATE EXTENSION METHOD WAS USED TO EXTEND THE NLG. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NOSE LANDING GEAR LOCK ACTUATOR.

Part: SLIDE — HUNG UP (R4 DOOR) · airframe 55,365 hrs · 22,471 cycles

CLT - EES - R-4 DOOR SLIDE BUSTLE HUNG UP IN DOOR FRAME NOT ALLOWING DOOR SLIDE TO PROPERLY INFLATE. ONCE BUSTLE WAS FREED SLIDE DEPLOYED IN 5 SECONDS. REPLACED R-4 DOOR ESCAPE SLIDE IAW JOB CARD 19L80025002.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT)

DUB FLT 722 EN ROUTE PHL TO DUB. ON APPROACH TO DUB, THE CREW RECEIVED AN EICAS MESSAGE FOR NLG DISAGREE, AND A NLG DOOR DISAGREE, ALONG WITH NO GREEN LIGHT ON THE PANEL. THE CREW PERFORMED A MANUAL (OR ALTERNATE) GEAR EXTENSION. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACTION PENDING.

Part: PACKING — LEAKING (SEQUENCE VALVE)

PHL FLT 1046 - EN ROUTE TPA TO PHL. DURING APPROACH, RECEIVED EICAS MESSAGE FOR GEAR DISAGREE NOSE GEAR DOOR, WITH NO NOSE GEAR GREEN LIGHT. THE GEAR WAS CYCLED, AND OPERATED NORMALLY ON THE SECOND ATTEMPT. MAINTENANCE REPLACED THE NOSE LANDING DOOR OPERATED SEQUENCE VALVE. OPERATIONALLY CHECKED OK. PRELIMINARY INSPECTION FOUND UNIT TO BE LEAKING FROM SEALS ON RETAINER (80) AND LEAKING INTERNALLY. TEARDOWN PROCEDURE FOUND ALL PACKING'S AND SEALS WORN OR DAMAGED. SPOOL SLEEVE ASSY HAS WEAR MARKS. REPLACE ALL DEFECTED ITEMS.

Part: BELLOWS — FAILED (FUEL FLOW GOVERN)

PIT - FLT 739 EN ROUTE PHL TO PIT. AT FL 220, THE AIRCRAFT EXPERIENCED A THROTTLE SPLIT OF ABOUT FIVE INCHES BETWEEN ENGINES 1 AND 2. THE MAX EPR ON THE RIGHT ENGINE WAS 1.19 AT THE FIREWALL. THE LEFT ENGINE HAD NORMAL READINGS. THE CREW DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE HP FUEL PUMP AND FUEL FLOW GOVERNOR. BASED ON SHOP FINDINGS, THE FUEL FLOW GOVERNOR WAS DETERMINED TO BE AT FAULT. ALT BIAS BELLOWS ASSEMBLY WAS INOPERATIVE/FAILED TEST.

Part: FUSE — BLOWN (EMERGENCY LIGHT)

PHL - MAINTENANCE REPORTED THE L3 DOOR EXTERIOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED A BLOWN FUSE IN POWER SUPPLY. OPERATIONAL CHECK GOOD.

Part: POWER UNIT — INOPERATIVE (FLASHLIGHT)

PHL - FLASHLIGHT, FWD FLIGHT ATTENDANT STATION WAS INOPERATIVE. REPLACED POWER UNIT AT FWD F/A SEAT FLASHLIGHT.

Part: FLAP — DELAMINATED (RT WING) · airframe 52,142 hrs · 21,583 cycles

CLT - C2 - MAJOR REPAIR - DELAMINATION ON RIGHT WING INBOARD MAIN FLAP TRAILING EDGE AT OUTBOARD END. REPAIRED RIGHT WING INBOARD MAIN FLAP TRAILING EDGE AT OUTBOARD END IAW B757 SRM 57-53-01 & 51-70-10.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 50,274 hrs · 20,869 cycles

MCO/PHL - RON MAJOR REPAIR - CRACK ON AFT CARGO DOOR FRAME FORWARD UPPER STOP FITTING. REPLACED AFT CARGO DOOR FRAME FORWARD UPPER STOP FITTING IAW B757 AMM 52-34-02-4.

Part: LIGHT — INOPERATIVE (L2 DOOR)

PHL - THE L2 DOOR ARMED LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED BURNED OUT BULB ON L2 DOOR ARM INDICATOR.

Part: WIRE — SHORTED (CABIN) · airframe 46,878 hrs · 19,501 cycles

MAINTENANCE FOUND R1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND POWER WIRE AT LIGHT SHORTED TO GROUND. REPOSITIONED WIRE, NO FURTHER FAULTS.

Part: SLIDE — LOW PRESSURE (L1 DOOR)

MCO - MAINTENANCE REPORTED THE L1 DOOR ESCAPE SLIDE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE. AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,198 hrs · 18,771 cycles

MAINTENANCE FOUND THE R1 SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY.